Cessna 402C - Page 234

SECTION 7
AIRPLANE & SYSTEMS DESCRIPTIONS
(~Oi,402C
3. Opening the dOQr will turn the lights on unless the timer extin-
guished the lights, in which case, one movement of the door switch
is also required in order to turn the lights on.
4.
With the cabin door open, the lights will always be on unless the
timer has turned them off. Movement 'of the door switch is required
to reset the lights to on for an additional 15 minutes. ~,
5. Closing the door will extinguish the lights only if the system is
switched off. If the system is on, the timer must continue to run
down to extinguish the lights.
Cockpit lighting is provided by the instrument panel floodlight, instru-
ment postl ights and overhead map 1i ghts . All cockpit 1ights a re va ri ab1e
intensity. Except for the instrument panel floodlight and the map lights,
lighting intensity is controlled by rheostats on the top of the control ~
pedestal, see Figure 7-19. The instrument panel floodlight and map lights
are controlled by rheostats on the overhead console, see Figure 7-2.
r--------
NOTE
---------.
I
The master panel lighting switch must be positioned
to DAY during daylight operations to insure adequate
illumination of the annunciator panel lights.
Individual reading lights and controls, see Figure 7-19, are provided in
the cabin for each passenger seat.
CABIN LIGHTING AND CONTROLS
OXYGEN OUTLET
READING LIGHT
AND CONTROL ___
----~
CABIN DOORWAY
LIGHT CONTROL
OVERHEAD
DIRECTIONAL
AIR VENT
8
/
lIf
<.\
K \~ ,
,
UPPER CABIN DOOR
LOCKED INDICATOR
CABIN DOORWAY FLOODLIGHT
UPPER DOOR LATCH
LOCK PLATE
LOWER DOOR LATCH
UPPER CARGO
DOOR LATCH
DOOR LATCHING
STOWAGE POCKET
LOWER CARGO
DOOR LATCH
OVERHEAD PASSENGER
CONTROL PANEL (TYPICAL)
5214P5025
5214PS027
Figure 7-20
1 November 1979
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